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Sting interference effects as determined by measurements of dynamic stability derivatives, surface pressure, and base pressure for Mach numbers 2 through 8

Title:Sting interference effects as determined by measurements of dynamic stability derivatives, surface pressure, and base pressure for Mach numbers 2 through 8
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Note:Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980
  
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Subject:Hypersonic wind tunnels
Subject:Interference (Aerodynamics)
Subject:Supersonic wind tunnels
Subject:Wind tunnel testing
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